Integrated Guidance Navigation and Control Using High-Order Sliding Mode Control for a Missile Interceptor
Author:
Affiliation:
1. University of Alabama, Huntsville
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1121
Reference27 articles.
1. Integrated missile guidance law and autopilot design using linear optimal control
2. Integrated Guidance and Control of Moving-Mass Actuated Kinetic Warheads
3. Optimal Fixed-Interval Integrated Guidance-Control Laws for Hit-to-Kill Missiles
4. Integrated Estimation, Guidance, and Control System Design Using Game Theoretic Approach
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1. Model Predictive Control With Wind Preview for Aircraft Forced Landing;IEEE Transactions on Aerospace and Electronic Systems;2023-08
2. RLV integrated guidance and control based on adaptive high-order sliding mode;Nonlinear Dynamics;2023-07-13
3. Robust extended state observer-based three dimensional integrated guidance and control design for interceptors with impact angle and input saturation constraints;ISA Transactions;2020-09
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